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REVISION RECORD
REVISION No. ISSUE DATE INCORPORATED BY DATE
Original 20 February 2004
Revision 1 30 May 2005
Revision 2 30 June 2005
Revision 3 30 September 2005
Revision 4 31 July 2006
Revision 5 26 November 2007
Revision 6 30 April 2009
Revision 7 6 January 2012
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REVISION HIGHLIGHTS
Revision 1
Guidance Base documents updated.
ATA 27 Flight Controls
27-53-02 Slat/Flap Actuator Control Electronic New Supplement entry to indicate that they must
(SF-ACE) Channels be operative.
ATA 32 Landing Gear
32-33-01 Landing Gear Control Lever Locking New Supplement entry to indicate that it must be
System operative.
ATA 34 Navigation
34-31-00 Radar Altimeter System New Supplement entry to align rectification
period with that for an inoperative GPWS.
34-41-00 Ground Proximity Warning System New Supplement entry to align with JAA policy
and to prevent dispatch in case of EGPWS
continuous warnings or cautions.
Revision 2
Revision 2 has been primarily issued to reflect the incorporation of the EMBRAER 175 model as
addressed in the revised ANAC MMEL at Revision 2.
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Revision 3
Definitions Included reference to Extended Overwater Operations.
ATA 52 Flight Controls
52-00-00 Passenger and Service Doors Removed proviso (a) according to TGL 26.
52-21-00 Overwing Escape Hatch New entry applicable to EMBRAER 190 only.
52-70-00 Door Position Indication Changed the number installed and required for dispatch to
on MFD and associated accommodate the EMBRAER 170 and EMBRAER 190
EICAS Message models.
Revision 4
Revision 4 has been issued to reflect the incorporation of the EMBRAER 195 model as addressed in the
revised ANAC MMEL at Revision 4.
ATA 22 AUTO FLIGHT CONTROL SYSTEM
22-10-14 Yaw Damper Channels Removed from JAA Supplement.
22-10-16 Flight Director Channels Removed from JAA Supplement.
22-11-02 Autopilot/TrimDisengage Updated according to ANAC Rev. 4.
(AP/TRIM DISC) Buttons
ATA 25 EQUIPMENT/FURNISHINGS
25-20-07 Passenger Convenience Remained in accordance with the ANAC previous Rev. 3.
Item(s) JAA/EASA has not established a policy for Non-Essential
Furnishings.
ATA 34 NAVIGATION
34-31-00 Radar Altimeter System Removed reference to FADEC version.
34-41-00 Ground Proximity Warning Deleted proviso referencing predictive windshear
System (GPWS) as it is not installed on these aircraft. Changed proviso b)
for a NOTE.
ATA 52 DOORS
52-21-00 Overwing Escape Hatch Included EMBRAER 195.
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Revision 5
Definitions Added Definition 28 to EASA regulations for ETOPS.
ATA 22 AUTO FLIGHT CONTROL SYSTEM 22-11-02 Autopilot/Trim Disengage
(AP/TRIM DISC) Buttons
Removed from JAA Supplement. Thus, relief is valid in
accordance with ANAC MMEL.
ATA 23 COMMUNICATIONS
23-11-00 High Frequency (HF)
Communication System
Inclusion in accordance with TGL 26.
ATA 25 EQUIPMENT/FURNISHINGS 25-11-01 Pilot Seats: Vertical Power
Seat Adjustment System
25-61-00 Emergency Locator
Transmitter (ELT) System
Revised in accordance with TGL 26.
25-65-00 Emergency Evacuation
Slides System
Revised in accordance with TGL 26.
ATA 28 FUEL 28-41-00 Fuel Quantity Indication on
MFD
Removed from JAA Supplement. Thus, relief is valid in
accordance with ANAC MMEL.
ATA 34 NAVIGATION 34-42-00 Weather Radar System:
Stabilization Function
Changed proviso for clarification.
ATA 35 OXYGEN
35-20-00 Passenger Oxygen System New item in JAA Supplement.
ATA 52 DOORS 52-00-00 Passenger and Service
Doors
Revised in accordance with TGL 26.
52-00-30 Passenger and Service
Doors Emergency Opening
Assisting System
Revised in accordance with TGL 26.
52-21-00 Overwing Escape Hatch Revised in accordance with TGL 26.
Editorial correction on pages S52-2, S52-.3, S52-4, S52-6 and S52-8.
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Revision 6
This revision reflects the incorporation of the 190-100 ECJ (Lineage 1000) model as addressed in the
ANAC MMEL at Revision 6.
Preamble Revised text to clarify “Rectification Interval Extensions”
Definitions Revised several references from JAR-OPS 1 to EU-OPS.
Revised Definition 28 and added the ECJ model ETOPS approval.
ATA 25 EQUIPMENT/FURNISHINGS
25-65-00 Emergency Escape Slides Added restriction to ECJ model.
ATA 26 FIRE PROTECTION
26-10-01 Lavatory Smoke Detection
System
New item in JAA Supplement.
ATA 34 NAVIGATION 34-11-00 Integrated Electronic
Standby System (IESS)
Added a new condition (5) according to ANAC
MMEL.
34-31-00 Radar Altimeter System Added new remarks for ECJ models.
ATA 44 CABIN SYSTEMS 44-13-00 Cabin Service Interphone
System
Added restriction to ECJ model.
ATA 46 INFORMATION SYSTEMS 46-20-00 Electronic Flight Bag Added new item according to TGL 26.
ATA 52 DOORS 52-00-00 Passenger and Service
Doors
Added restriction to ECJ model.
52-00-30 Passenger and Service
Doors Emergency Opening
Assisting System
Added restriction to ECJ model.
52-21-00 Overwing Escape Hatch Added restriction to ECJ model.
52-31-20 Fwd (Aft) Cargo Door
Green Inciators
New supplement entry to indicate that all must be
operative.
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Revision 7
This Revision reflects the JAA Supplement conversion to an EASA Supplement.
Preamble Updated text to CLARIFY
Guidance “Guidance for use of this Supplement” updated
ATA 23 COMMUNICATIONS
23-51-02 Cockpit Speakers New item in EASA Supplement.
23-51-08 Flight Deck
Headsets/Headphones
Revised in accordance to TGL 26.
ATA 25 EQUIPMENT/FURNISHINGS
25-61-00 Emergency Locator
Transmitter (ELT) System
Removed word system from item title.
ATA 27 FLIGHT CONTROLS 27-03-04 Pitch Trim System Channel
Cutout Pushbutton
Illumination
New item in EASA Supplement.
27-53-02 Slat/Flap Actuator Control
Electronic (SF-ACE)
Channels
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
ATA 29 HYDRAULIC POWER
29-11-04 Systems 1 and 2 Filter
Manifold Differential
Pressure Indicator
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
29-11-06 Systems 1 and 2 Case Drain
Differential Pressure
Indicator
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
29-12-02 System 3 Filter Manifold
Differential Pressure
Indicator
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
29-12-04 System 3 Case Drain
Differential Pressure
Indicator
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
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ATA 34 NAVIGATION
34-11-00 Integrated Electronic
Standby System
Removed from EASA Supplement. Thus, relief is valid
in accordance with ANAC MMEL.
34-31-00 Radar Altimeter System Added request for deactivation of the system.
34-41-00 Ground Proximity Warning
System
Updated according to ANAC Rev. 7 and TGL 26.
34-61-00 Flight Management System Revised in accordance to TGL 26.
ATA 46 INFORMATION SYSTEMS
46-21-00 Electronic Flight Bag
Systems
Updated according to ANAC Rev. 7.
ATA 50 CARGO AND ACCESSORY COMPARTMENTS 50-22-02 Cargo / Baggage Nets New item in EASA Supplement.
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TABLE OF CONTENTS
REVISION HIGHLIGHTS
LIST OF EFFECTIVE PAGES
PREAMBLE
DEFINITIONS
GUIDANCE MATERIAL
21 AIR CONDITIONING
22 AUTO FLIGHT CONTROL SYSTEM
23 COMMUNICATIONS
24 ELECTRICAL POWER
25 EQUIPMENT/FURNISHINGS
26 FIRE PROTECTION
27 FLIGHT CONTROL
28 FUEL
29 HYDRAULIC POWER
30 ICE AND RAIN PROTECTION
31 INDICATING/RECORDING SYSTEMS
32 LANDING GEAR
33 LIGHTS
34 NAVIGATION
35 OXYGEN
36 PNEUMATIC
38 WATER AND WASTE
44 CABIN SYSTEMS
45 CENTRAL MAINTENANCE SYSTEMS (CMS)
46 INFORMATION SYSTEMS
49 AIRBORNE AUXILIARY POWER
50 CARGO AND ACCESSORY COMPARTMENTS
52 DOORS
73 ENGINE FUEL AND CONTROL
74 IGNITION
77 ENGINE INDICATING
78 EXHAUST
79 OIL
80 STARTING
Note: The above is a list of the applicable ATA Chapters for which MMEL relief could be amended by
this supplement. Check the list of effective pages to determine if there are active pages in any
specific chapter.
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List of Effective Pages
Page Title Revision Date
ii Title Sheet Revision 7 6 January 2012
iii Approval Sheet Revision 7 6 January 2012
v Revision Record Revision 7 6 January 2012
vii Revision Highlights Revision 7 6 January 2012
viii Revision Highlights Revision 7 6 January 2012
ix Revision Highlights Revision 7 6 January 2012
x Revision Highlights Revision 7 6 January 2012
xi Revision Highlights Revision 7 6 January 2012
xii Revision Highlights Revision 7 6 January 2012
xiii Table of Contents Revision 7 6 January 2012
xv List of Effective Pages Revision 7 6 January 2012
xvi List of Effective Pages Revision 7 6 January 2012
xviii Preamble Revision 7 6 January 2012
xix Preamble (Cont.) Revision 7 6 January 2012
xx Definitions and Symbology Revision 7 6 January 2012
xxi Definitions and Symbology (Cont.) Revision 7 6 January 2012
xxii Definitions and Symbology (Cont.) Revision 7 6 January 2012
xxiii Definitions and Symbology (Cont.) Revision 7 6 January 2012
xxiv Guidance for Use of this Supplement Revision 7 6 January 2012
S22-1 Auto Flight Control System Revision 5 26 November 2007
S23-1 Communications Revision 7 6 January 2012
S25-1 Equipment/Furnishings Revision 5 26 November 2007
S25-2 Equipment/Furnishings Revision 7 6 January 2012
S26-1 Fire Protection Revision 6 30 April 2009
S27-1 Flight Control Revision 7 6 January 2012
S29-1 Hydraulic Power Revision 7 6 January 2012
S30-1 Ice and Rain Protection Original 20 February 2004
S31-1 Indicating/Recording Systems Original 20 February 2004
S33-1 Lights Original 20 February 2004
S34-1 Navigation Revision 7 6 January 2012
S34-2 Navigation Revision 7 6 January 2012
S34-3 Navigation Revision 7 6 January 2012
S34-4 Navigation Revision 7 6 January 2012
S34-5 Navigation Revision 5 26 November 2007
S34-6 Navigation Revision 7 6 January 2012
S34-7 Navigation Revision 7 6 January 2012
S35-1 Oxygen Revision 6 30 April 2009
S44-1 Cabin Systems Revision 6 30 April 2009
S46-1 Information Systems Revision 7 6 January 2012
S50-1 Cargo and Accessory Compartments Revision 7 6 January 2012
S52-1 Doors Revision 6 30 April 2009
S52-2 Doors Revision 6 30 April 2009
S52-3 Doors Revision 5 26 November 2007
S52-4 Doors Revision 5 26 November 2007
S52-5 Doors Original 20 February 2004
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List of Effective Pages (Cont.)
Page Title Revision Date
S52-6 Doors Revision 5 26 November 2007
S52-7 Doors Original 20 February 2004
S52-8 Doors Revision 5 26 November 2007
S52-9 Doors Original 30 September 2005
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PREAMBLE
The following is applicable for operators under European operating regulations (EU-OPS or Part-OPS).
The regulations require that all equipment installed on an aircraft in compliance with the Airworthiness
Code and the Operating Requirements must be operative. However, the requirements also permit the use
of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not
necessary in the interests of safety under all operating conditions. Experience has shown that with the
various levels of redundancy designed into aircraft, operation of every system or installed component may
not be necessary when the remaining operative equipment can provide an acceptable level of safety.
A Master Minimum Equipment List (MMEL) is developed by the Type Certificate Holder to improve
aircraft utilization and thereby provide more convenient and economic air transportation for the public.
The EASA MMEL includes those items of equipment related to airworthiness and operating requirements
and other items of equipment which EASA finds may be inoperative and yet maintain an acceptable level
of safety by appropriate conditions and limitations; it does not contain obviously required items such as
wings, flaps, and rudders.
The MMEL is the basis for development of individual operators’ MELs, which take into consideration the
operator’s particular aircraft equipment configuration and operational conditions. An operator’s MEL may
differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator’s
MEL, when approved, permits operation of the aircraft with inoperative equipment.
Equipment not required by the operation being conducted and equipment in excess of the requirements is
included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the
Airworthiness Directives or any other Mandatory Requirement. It is important to remember that all
equipment related to the airworthiness and the operating requirements of the aircraft not listed on the
MMEL must be operative.
Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating
procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level
of safety is maintained.
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PREAMBLE (Cont.)
The MEL is intended to permit operation with inoperative items of equipment for a period of time until
rectifications can be accomplished. It is important that rectifications be accomplished at the earliest
opportunity. In order to maintain an acceptable level of safety and reliability, the MMEL establishes
limitations on the duration of, and conditions for operation with inoperative equipment. The operator may
be permitted, by their competent authority, a one-time extension of the applicable rectification intervals B,
C or D for the same duration as that specified in their MEL. This extension policy has been taken into
account during the development of this document.
When an item of equipment is discovered to be inoperative, it is reported by making an entry in the
Aircraft Maintenance Record/Logbook as prescribed by the applicable regulations. The item is then either
rectified or may be deferred per the MEL or other approval means acceptable to the competent Authority
prior to further operation. MEL conditions and limitations do not relieve the operator from determining
that the aircraft is in a condition for safe operation with items of equipment inoperative.
When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook
entry, or other approved documentation is issued as prescribed by the applicable regulations. Such
documentation is required prior to operation with any item of equipment inoperative.
Operators are responsible for exercising the necessary operational control to ensure that an acceptable
level of safety is maintained. The exposure to additional failures during continued operation with
inoperative systems or components must also be considered. Wherever possible, account has been taken in
this MMEL of multiple inoperative items. However, it is unlikely that all possible combinations of this
nature have been accounted for. Therefore, when operating with multiple inoperative items, the inter-
relationships between those items and the effect on aircraft operation and crew workload must be
considered.
Operators are to establish a controlled and sound rectification program including the parts, personnel,
facilities, procedures and schedules to ensure timely rectification. This program should identify the
actions required for Maintenance discrepancy messages.
WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,
DEFINITIONS AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS
REQUIRED.
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DEFINITIONS AND SYMBOLOGY
1) System numbers are based on Air Transport Association (ATA) number 2200.
2) “Item” (column 1) means the equipment component or function of a system, listed in the Item
Column.
3) Rectification Interval: a letter designator is inserted in Column 2. All deferred MMEL items must be
repaired or replaced at or prior to the rectification times established by the following letter
designators:
- Category A - Items in this category must be rectified within the time interval specified in the remarks
column.
- Category B - Items in this category must be rectified within three consecutive calendar days,
excluding the day the malfunction was recorded in the logbook. For example, if it were recorded at
10 am. on December, 11th, the three day interval would begin at midnight the 11th and end at
midnight the 14th.
- Category C - Items in this category must be rectified within ten consecutive calendar days, excluding
the day the malfunction was recorded in the logbook. For example, if it were recorded at 10 am. on
December, 11th, the ten day interval would begin at midnight the 11th and end at midnight the 21st.
- Category D - Items in this category must be repaired within one hundred and twenty consecutive
calendar days (2880 hours), excluding the day the malfunction was recorded in the logbook.
4) The number in column 3 indicates the number of listed items normally installed on the aircraft. This
number reflects the aircraft type certificated configuration, and therefore, required for all flight
operations, except as provided in columns 4 and 5. The dash (-) symbol in column 3 indicates a
variable number of the item installed, depending on the aircraft configuration. The dash symbol (-) in
column 4 indicates a variable number of items are required to be operative for dispatch, as described
in column 5.
NOTE: The operator’s MEL must indicate the actual number installed on their aircraft and the actual
number required for dispatch.
5) References may be given in column 5 to bring attention to certain interrelationships between the
subject item and other MMEL items or AFM material. These references are intended to assist with
compliance, but do not relieve the operator of responsibility for determining such interrelationships as
stated in the Preamble. The provisos included in column 5 shall be complied with.
6) “Note” in column 5 indicates additional information and references for crewmember or maintenance
consideration. Notes are not part of the provisos.
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DEFINITIONS AND SYMBOLOGY (Cont.)
7) “As required by local regulations/Operating Requirements” means that the associated item must
comply with EU-OPS or any other legislation in force during the flight. Operators should refer to
JAR-OPS MEL Policy Document (JAA Administrative and Guidance Material, Section Four:
Operations, Part Three: Temporary Guidance Leaflet 26) for suitable alleviations and rectification
intervals based upon the required equipment identified in EU-OPS, subparts K and L.
8) “Inoperative” means a condition in which a listed item of equipment is malfunctioning to the extent
that it does not accomplish its intended purpose, or is not consistently functioning within its designed
operating limit(s) or tolerance(s). Unless individually permitted to be inoperative, a component or
function of a system which is inoperative implies that the system is inoperative (warning/caution
systems associated with the inoperative system must be operative unless relief is specifically
authorized by the MMEL).
9) “Inoperative EICAS Message” means a message that is erroneously displayed.
10) Each inoperative item must be placarded to inform crewmembers of the equipment condition. As
much as possible, placards should be located adjacent to the control or indication of the affected item,
however, unless otherwise specified herein, placard wording and location will be determined by the
operator.
11) “VFR” (Visual Flight Rules) is as defined in EU-OPS.
12) “VMC” ( Visual Meteorological Conditions ) - The atmospheric environment is such that would allow
the flight to proceed under visual flight rules applicable to the flight.
13) “Icing Conditions” means an atmospheric environment that may cause ice to form on the aircraft or in
the engines.
14) “Visible Moisture” means an atmospheric environment containing water in any form that can be seen
in natural or artificial light; for example: clouds, fog, rain, sleet, hail, or snow.
15) “Secured” and “Deactivated” means that the specified component must be put into an acceptable
condition for safe flight. An acceptable method of securing or deactivating will be established by the
operator.
NOTE: EMBRAER publishes the Dispatch Deviations Procedures Manual, which contains acceptable
procedures for MMEL compliance. 16) “Passenger Convenience Items” means those items related to passenger convenience, comfort or
entertainment such as, but not limited to, galley equipment, movie equipment, ashtrays, stereo
equipment, overhead reading lamps, etc.
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DEFINITIONS AND SYMBOLOGY (Cont.)
17) “Flight hours” for MMEL purposes means the time from the moment the aircraft leaves the surface of
the earth until it touches it at the next point of landing (i.e., takeoff to landing time).
18) “Flight day” - a 24-hour period (from midnight to midnight) during which at least one flight is
scheduled for the affected aircraft.
19) “Day of discovery” is the calendar day the equipment was found to be malfunctioning.
20) "(M)" symbol indicates a requirement for a specific maintenance procedure which must be
accomplished prior to operation with the listed item inoperative. Normally these procedures are
accomplished by maintenance personnel; however, other personnel may be qualified and authorized
to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use
of tools or test equipment should be accomplished by maintenance personnel. The satisfactory
accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility
of the operator. Appropriate procedures are required to be published as part of the operator's manual
or MEL.
21) "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished
in planning for and/or operating with the listed item inoperative. Normally these procedures are
accomplished by the flight crew; however, other personnel may be qualified and authorized to
perform certain functions. The satisfactory accomplishment of all procedures, regardless of who
performs them, is the responsibility of the operator. Appropriate procedures are required to be
published as part of the operator's manual or MEL.
22) Three asterisks (***) in column 1 indicates an item which is not required by the Airworthiness
Regulations, but may have been installed in the aircraft. It should be noted that neither this definition
nor the use of this symbol provide authority to install or remove an item from an aircraft.
23) The / symbol indicates “and/or”.
24) A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text
for the current revision of that page only. The change bar is dropped at the next revision of that page.
25) A change bar adjacent to the page number indicates that the page was renumbered only and that no
change was made in the text.
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DEFINITIONS AND SYMBOLOGY (Cont.)
26) “Combustible material” is defined as being a material which is capable of catching fire and burning.
NOTE: When an MMEL item specifies that only non-combustible materials shall be carried, it is
operator’s responsibility to determine that all material (including packages, containers,
contents, etc.) in the compartment is of a non-combustible nature. If it cannot be determined
whether any proposed cargo is non-combustible, it must not be loaded in the compartment.
27) “Extended Overwater Flight”: Refer to EU-OPS Subpart K for definition.
28) "ER" refers to extended range operations of a two-engine airplane (ETOPS) which has a type design
approval for ER operations (ETOPS) and complies with the provisions of AMC 20-6 “Extended
Range Operations with Two-Engine Aeroplanes ETOPS Certification and Operation”, as amended
and EU-OPS as amended.
NOTE: Only EMBRAER 190 ECJ (Lineage 1000) model is approved for ETOPS by EASA.
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SUPPLEMENT
EMBRAER 170/175/190/195
GUIDANCE FOR USE OF THIS SUPPLEMENT
1. This Supplement is applicable to all ERJ 170-100, ERJ 170-200, ERJ 190-100, ERJ 190-100 ECJ
and ERJ 190-200 models which have the commercial designation of EMBRAER 170,
EMBRAER 175, EMBRAER 190, LINEAGE 1000 and EMBRAER 195, respectively.
2. This Supplement defines the standard of MMEL recommended for the above aircraft type by the
European Aviation Safety Agency (EASA) by identifying the differences from the ANAC
MMEL.
3. The information presented in the ANAC MMEL for the aircraft type is acceptable to EASA
except where superseded by an item in this supplement.
NOTE: Items within this supplement will use the same reference number as the corresponding
item in the ANAC MMEL. Where an item in this supplement does not appear in the ANAC
MMEL, the number will be preceded by “E”, and the sequential reference will commence from
“1” again. (e.g. E52-1 would be the first EASA specific item in ATA Chapter 52). Such items will
be placed at the end of the related chapter.
4. Unless otherwise stated within this Supplement, the Definitions contained in the ANAC MMEL
are applicable. However, EASA equivalents must be assumed in reading and applying both.
5. This supplement is based upon the ANAC approved EMBRAER 170/175/190/195 MMEL at
Revision 8 dated 17 August 2011. Additional MMEL alleviation provided by later issues of the
ANAC MMEL must not be used until this EASA Supplement has been updated to confirm that
issue as the base document.
6. The text presented in bold format within this document highlights parts of the EASA MMEL
Supplement entry which differ from the ANAC MMEL entry.
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
xxv
Revision: 7
Date: 6 January 2012
SUPPLEMENT
EMBRAER 170/175/190/195
INTENTIONALLY LEFT BLANK
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S22-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
s (3) Number installed
(4) Number required for dispatch
22 Auto Flight Control System
(5) Remarks or Exceptions
-10-00 Autopilot Channels B 2 0 May be inoperative provided operations do not require their
use.
NOTE: this system is required to be operative for RVSM
operations.
-11-01 Guidance Panel (GP)
3) Autopilot (AP) Button B 1 0 May be inoperative provided operations do not require its use.
NOTE: this system is required to be operative for RVSM
operations.
15) Altitude Hold (ALT)
Mode Button
C 1 0 May be inoperative provided operations do not require its use.
NOTE: this system is required to be operative for RVSM
operations.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S23-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
(5) Remarks or Exceptions
23 Communications
-11-00 High Frequency (HF)
Communication System
***
D - - Any in excess of those required for the intended route may
be inoperative.
C - 1 (O) Any in excess of one may be inoperative for flight on a
route that requires two Long Range Communication
Systems, provided:
a) SATCOM air-ground communications with relevant
Air Navigation Service Provider(s) are available over the
route to be flown,
b) SATCOM Voice or Data transfer functions are
operative,
c) Prior to each flight, coordination with the appropriate
Air Navigation Service Provider(s) is established where
INMARSAT codes, or equivalent, are not available whilst
using SATCOM voice function, and
d) Alternate communication procedures are established
and used.
NOTE 1: SATCOM is to be used only as a backup to
normal HF communications unless otherwise authorized
by the appropriate Air Navigation Service Provider(s).
NOTE 2: For all routes, consider the need for TCAS.
-51-00 Cockpit/Cabin Service
Interphone System
- - - As required by Operating Requirements.
-51-02 Cockpit Speakers C 2 0 May be inoperative provided procedures do not require its
use.
-51-08 Headset with Boom
Microphone
D - - Any in excess of one headset (including boom
microphone) for each required crew member on
flight deck duty may be inoperative or missing.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S25-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
25 Equipment/Furnishings
-11-01 Pilot Seats
1) Vertical Power Seat
Adjustment System
2) Vertical Manual Seat
Adjustment System
7) Recline Function
D
B
B
B
2
2
2
2
0
0
0
0
(5) Remarks or Exceptions
(M) May be inoperative provided:
(a) Affected system is deactivated, and
(b) Vertical manual seat adjustment system operates normally.
May be inoperative provided:
(a) Affected seat has failed in a position that permits normal
pilot visibility,
(b) Full flight control movement is available, and
(c) Seat is acceptable to the affected flight crew member.
May be inoperative provided vertical power seat adjustment
system operates normally.
May be inoperative provided seat is acceptable to the affected
crewmember.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S25-2
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
25 Equipment/Furnishings
(5) Remarks or Exceptions
-11-02 Observer Seat (Including
Associated Equipment)
- - - As required by Operating Requirements.
-20-07 Passenger Convenience
Item(s)
- 0 Passenger convenience items, as expressed in this MMEL, are
those related to passenger convenience, comfort, or
entertainment such as, but not limited to, galley equipment,
movie equipment, ash trays, stereo equipment, overhead
reading lamps. Items addressed elsewhere in this document
shall not be included. (M) and (O) procedures may be required
and included in the air carrier's appropriate document.
NOTE: Exterior lavatory door ashtrays are not considered
convenience items.
61-00 Emergency
*** Locator Transmitter
(ELT)
1) Survival Type ELTs D - - Any in excess of the minimum required may be missing or
inoperative provided the inoperative equipment is
placarded inoperative, removed from the installed
location, and placed out of sight so it cannot be mistaken
for a functional unit.
2) Fixed ELTs A - 0 May be inoperative provided repairs are made within 6
further flights or 25 flying hours, whichever occurs first.
D - - Any in excess of those required by local regulations may be
inoperative.
-62-01 Emergency Medical
Equipment
- - - As required by Operating Requirements.
-65-00 Emergency Evacuation
Slides System
(except ECJ model)
A
4
3
(M) (O) One may be inoperative or missing for a maximum
of 5 flights provided:
(a) Associated door is considered inoperative. Refer to item
52-00-00 Passenger and Service Doors.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 6
DATE: 30 April 2009
PAGE
S26-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
26 Fire Protection
-10-01 Lavatory Smoke
Detection System
(ERJ-190-100ECJ)
1) Fwd and Mid Cabin
Lavatory
C - - (M)(O)May be inoperative provided:
a) Lavatory waste receptacle is empty, and
b) Lavatory door is locked closed and placarded
"INOPERATIVE - DO NOT ENTER".
2) VIP Cabin Lavatory C - - (M)(O)May be inoperative provided:
a) Lavatory waste receptacle is empty, and
b) Lavatory door is locked closed and placarded
"INOPERATIVE - DO NOT ENTER".
NOTE: These provisos are not intended to prohibit lavatory
use or inspections by crewmembers.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S27-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
27 Flight Control
-03-04 Pitch Trim System
Channel Cutout
Pushbutton Illumination
-41-01 Pitch Trim Position
Indication on EICAS
-53-02 Slat/Flap Actuator
Control Electronic
(SF-ACE) Channels
C
A
1
1
0
0
(5) Remarks or Exceptions
(M) May be inoperative provided:
(a) Pitch trim channels are verified operative, and
(b) Associated pushbutton is verified operative.
(M) (O) May be inoperative for one flight only provided
horizontal stabilizer position is set by means of markings on
tail cone before each flight.
(deleted from supplement on Revision 7)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S29-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
29 Hydraulic Power
-11-04 Systems 1 and 2 Filter
Manifold Differential
Pressure Indicators
-11-06 Systems 1 and 2 Case
Drain Differential
Pressure Indicators
-12-02 System 3 Filter Manifold
Differential Pressure
Indicators
-12-04 System 3 Case Drain
Differential Pressure
Indicators
(5) Remarks or Exceptions
(deleted from supplement on Revision 7)
(deleted from supplement on Revision 7)
(deleted from supplement on Revision 7)
(deleted from supplement on Revision 7)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 20 February 2004
PAGE
S30-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
30 Ice and Rain Protection
-41-00 Windshield Wiper
System
-
-
-
(5) Remarks or Exceptions
As required by Operating Requirements.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 20 February 2004
PAGE
S31-1
(1) System & Sequence Numbers
Item
(2)Rectification Interval
(3) Number installed
(4) Number required for dispatch
31 Indicating / Recording
Systems
-21-00 Clock System
1) Time Function on
Digital Clock
2) Time Function on
MFD Status Page
-31-00 Digital Voice Data
Recorder (DVDR)
System
C
C
A
-
1
2
2
-
0
1
0
-
(5) Remarks or Exceptions
May be inoperative provided at least one Time Function on
MFD Status Page operates normally.
May be inoperative provided:
(a) Time Function on Digital Clock operates normally,
(b) At least one Cockpit Voice Recorder (CVR) function
operates normally,
(c) The aeroplane does not exceed 8 further consecutive
flights, and
(d) Not more than 72 hours have elapsed since the Time
Function on the MFD Status Page was found to be
inoperative.
As required by Operating Requirements.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 4
DATE: 31 July 2006
PAGE
S32-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
32 Landing Gear
-33-01 Landing Gear Control
Lever Lock Solenoid
(5) Remarks or Exceptions
Item deleted.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 20 February 2004
PAGE
S33-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
33 Lights
-45-00 Red Beacon Lights
-
-
-
(5) Remarks or Exceptions
As required by Operating Requirements.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-11-00 Integrated Electronic
Standby System (IESS)
(5) Remarks or Exceptions
(1) Standby Attitude
Indication
C 1 0 May be inoperative provided not required by local regulations.
B 1 0 May be inoperative provided:
(a) All Display Units are operative, and
(b) Operations are conducted in Day VMC only, and in sight
of the ground.
(2) STD Baro Button
C 1 0 May be inoperative provided BARO knob on the IESS
operates normally.
(3) Brightness Buttons
C 2 0 May be inoperative provided brightness level is acceptable to
the crew.
(4) CAGE Button
B 1 0 (O) May be inoperative provided IESS is reinitialized before
each flight.
B 1 0 May be inoperative provided IESS attitude indication is
considered inoperative.
(5) VMO/MMO Barber
Pole
C 1 0 May be inoperative provided VMO Flag is displayed.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-2
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-31-00 Radar Altimeter System
-32-00 Very High Frequency
Navigation Systems
(VHF NAV)
(1) VOR/ILS Systems
(2) Marker Beacon
Systems
C
A
-
-
2
-
-
-
1
0
-
-
(5) Remarks or Exceptions
(M) May be inoperative provided:
(a) System is deactivated, and,
(b) Approach minimums or operating procedures do not
require its use.
(M) May be inoperative provided:
(a) System is deactivated,
(b) Approach minimums or operating procedures do not
require its use,
(c) Ground Proximity Warning System (GPWS) Modes 1-4,
Mode 5, Advisory Callouts and Windshear Mode are
considered inoperative,
(d) Traffic Alert and Collision Avoidance System (TCAS) is
considered inoperative,
(e) For ECJ models, the Internal Door Warning System is
considered inoperative,
(f) For ECJ models, the Iridium system is considered
inoperative, and,
(g) Repairs or replacements are carried out within 6
further flights or 25 flying hours or 2 calendar days,
whichever occurs first.
As required by Operating Requirements.
As required by Operating Requirements.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-3
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-41-00 Terrain Awareness
and Warning System
(TAWS)
1) Ground Proximity
Warning System
(GPWS)
a) Modes 1 to 4
b) Test Mode
A
C
A
C
A
1
1
4
4
1
0
0
0
0
0
(5) Remarks or Exceptions
(O) May be inoperative provided:
(a) Alternate procedures are established and used, and
(b) Repairs or replacements are carried out within 6
further flights or 25 flying hours or 2 calendar days,
whichever occurs first.
(O) May be inoperative provided:
(a) It is not required by local regulations, and
(b) Alternate procedures are established and used.
(O) May be inoperative provided:
(a) Alternate procedures are established and used, and
(b) Repairs or replacements are carried out within 6
further flights or 25 flying hours or 2 calendar days,
whichever occurs first.
(O) May be inoperative provided:
(a) It is not required by local regulations, and
(b) Alternate procedures are established and used.
(O) May be inoperative provided:
(a) GPWS is considered inoperative, and
(b) Repairs or replacements are carried out within 6
further flights or 25 flying hours or 2 calendar days,
whichever occurs first.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-4
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-41-00 Terrain Awareness
and Warning System
(TAWS)
c) Glideslope Deviation
(Mode 5)
*** d) Advisory Callouts
*** e) Windshear Warning
and Flight Guidance
System (Windshear
Mode)
*** 2) Terrain System -
Forward Looking
Terrain Avoidance
(FLTA) and
Premature Descent
Alert (PDA)
Functions
*** 3) Runway Awareness
and Advisory
System
C
C
B
C
C
B
C
2
2
2
-
1
1
1
1
0
0
0
0
0
0
(5) Remarks or Exceptions
May be inoperative provided it is not required by local
regulations.
May be inoperative.
(O) May be inoperative provided alternate procedures are
established and used.
NOTE: Check Flight Manual limitations for approach
minimums.
(O) May be inoperative provided alternate procedures are
established and used.
NOTE: Operator's alternate procedures should include
reviewing windshear avoidance and windshear recovery
procedures.
(O) May be inoperative provided alternate procedures are
established and used.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S34-5
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-42-00 Weather Radar System
1) Stabilization Function
-43-00 Traffic Alert and
Collision Avoidance
System II (TCAS II)
1) Resolution Advisory
(RA) Display
System(s)
2) Traffic Alert (TA)
Display System (s)
-
C
A
C
C
C
-
1
-
2
-
-
-
0
0
1
0
0
(5) Remarks or Exceptions
As required by Operating Requirements.
(M) May be inoperative provided:
(a) Antenna sweep is verified parallel to aircraft horizontal
plane, and
(b) Antenna tilt is operated manually.
(O) (M) May be inoperative provided the system is
deactivated and secured and:
(a) It is not reasonably practicable to repair before the
commencement of the flight, and
(b) If the aeroplane is intended to be flown in airspace in
which ACAS operation is required it may not fly for
more than 10 calendar days with the equipment
completely inoperative.
NOTE: Local airspace requirement may impose a
more restrictive rectification interval.
(O) May be inoperative on the non-flying pilot side.
(O) May be inoperative provided:
(a) All Traffic Alert (TA) display elements and voice
command audio functions are operative, and
(b) TA only mode is selected by the crew.
(O) One or more may be inoperative provided all installed
RA display and audio functions are operative.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-6
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-52-00 ATC Transponder and
Automatic Altitude
Reporting System
-61-00 Flight Management
System (FMS)
1) Navigation
Databases
NOTE: Database(s)
which is/are
out of date
is/are
considered to
be
inoperative.
D
C
D
C
C
A
-
-
2
-
-
-
-
0
1
0
1
0
(5) Remarks or Exceptions
As required by Operating Requirements. Any in excess of
those required may be inoperative.
(O) May be inoperative provided alternate procedures are
established and used.
May be inoperative provided procedures do nor require its
use.
(O) One or more may be inoperative for the intended
route where conventional (non-RNAV) navigation is
sufficient, provided:
(a) Current aeronautical information (e.g. charts) is
available for the entire route and for the aerodromes
to be used, and
(b) Navigation database information is disregarded.
Any in excess of one may be inoperative provided:
(a) The operative database must be up to date for routes,
departures, arrival and approach procedures that
require the use of navigation Database for RNAV, and
(b) This up to date Database is readily available to the
flight crew member(s) responsible for navigation.
(O) One or more may be out of date for a maximum of 10
calendar days provided:
(a) Area Navigation (RNAV) departure, arrival and
approach procedures do not depend on the data amended
in the current database cycle,
(b) Before each flight, current aeronautical information is
used to verify the database Navigation Fixes, the
coordinates, frequencies, status (as applicable) and
suitability of Navigation Facilities required for the
intended route, and
(c) Radio navigation aids, which are required to be flown
for departure, arrival and approach procedures and which
have been amended in the current database cycle, are
manually tuned and identified.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S34-7
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
34 Navigation
-61-00 Flight Management
System (FMS)
(Continued)
1) Navigation
Databases
(Continued)
NOTE: Database(s)
which is/are
out of date
is/are
considered to
be
inoperative.
A
-
0
(5) Remarks or Exceptions
(O) One or more may be out of date for a maximum of 10
calendar days provided:
(a) Conventional (Non-RNAV) departure, arrival and
approach procedures, when available, or ANSP assistance
are used as an alternative to RNAV procedures which
have been amended in the current database cycle,
(b) Before each flight, current aeronautical information is
used to verify the database Navigation Fixes, the
coordinates, frequencies, status (as applicable) and
suitability of Navigation Facilities required for the
intended route, and
(c) Radio navigation aids, which are required to be flown
for departure, arrival and approach procedures and which
have been amended in the current database cycle, are
manually tuned and identified.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S35-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
(5) Remarks or Exceptions
35 Oxygen
-20-00 Passenger Oxygen
System
B 1 0 (O) May be inoperative provided:
(a) Flight is not conducted over an area where the Minimum
Enroute Altitude is above 14000 ft MSL,
(b) Both air conditioning packs operate normally,
(c) Pressurization system operates normally,
(d) Flight is conducted at or below FL 250,
(e) Portable oxygen units are provided for all crew
members and for 10 percent of the passengers for
half an hour (supplemental oxygen), and
(f) Passengers are appropriately briefed.
B 1 0 (O) May be inoperative provided:
(a) Maximum altitude is limited to a pressure altitude of
10,000 ft MSL,
(b) All air-conditioning packs operate normally,
(c) All other components of the pressurization system
operate normally, and
(d) Passengers are appropriately briefed.
1) Automatic
Deployment System
C 1 0 (M) (O) May be inoperative provided:
a) Manual deployment (OVRD) system operates normally,
and
b) Flight is conducted at or below FL 300.
2) Passenger Oxygen
Dispensing Unit
C - 0 (M) May be inoperative with no flight altitude restriction
provided:
a) Affected seats are placarded and blocked to prevent
occupancy, and
b) Units operate normally at all usable lavatory and
flight attendant locations.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 6
DATE: 30 April 2009
PAGE
S44-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
44 Cabin Systems
(5) Remarks or Exceptions
-11-00 Passenger Address
-13-00 Cabin Service
Interphone System
(except ECJ model)
-13-01 Flight Attendant
Handset
-
-
-
-
-
-
-
-
-
As required by Operating Requirements.
As required by Operating Requirements.
As required by Operating Requirements.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S46-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
46 Information Systems
(5) Remarks or Exceptions
-21-00 Electronic Flight Bag
*** Systems (EFBs)
C - 0 (M)(O) May be inoperative provided alternate procedures
are established and used where operating procedures are
dependant upon the use of the affected EFB.
Note: Any EFB function which operates normally may be
used.
1) Mounting Device
C - 1 (M) (O) Any in excess of one may be inoperative provided
the affected EFB is secured by an alternative means.
C - 0 (M) (O) May be inoperative provided:
(a) The associated EFB is used in accordance with Class 1
EFB stowage criteria, and
(b) Alternate procedures are established and used where
operating procedures are dependant upon the use of the
affected EFB.
2) Data Connectivity
C - 1 (M) (O) Any in excess of one may be inoperative provided
an alternative means of data connectivity is used.
C - 0 (M) (O) May be inoperative provided alternate procedures
are established and used where operating procedures are
dependant upon the use of the affected EFB.
Note: Any EFB function which operates normally may be
used.
3) Power Connection
C - 1 (M) (O) Any in excess of one may be inoperative provided
an alternative power source is available and can be used
for the planned duration of use of the affected EFB.
C - 0 (M) (O) May be inoperative provided alternate procedures
are established and used.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 7
DATE: 6 January 2012
PAGE
S50-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
50 Cargo and Accessory
Compartments
(5) Remarks or Exceptions
-22-02 Cargo / Baggage Nets
***
D - 0 May be inoperative or missing provided associated cargo/
baggage compartment remains empty.
(except ECJ model)
D - 0 (O) May be inoperative or missing provided acceptable
cargo loading limits from an approved source, i.e., an
Approved Cargo Loading Manual, Cargo Handling
Manual or Weight and Balance document are observed.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 6
DATE: 30 April 2009
PAGE
S52-1
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
(5) Remarks or Exceptions
-00-00 Passenger and Service
Doors
(except ECJ model)
A 4 3 (M) (O) One may be inoperative for a maximum of 5
flights provided:
(a) The passenger number reduction and distribution
policy, and cabin safety procedures are established and
used,
(b) The affected emergency exit is closed and locked,
(c) A conspicuous barrier, strap or rope and a placard
stating “DO NOT USE” are placed across the affected
emergency exit prior to passenger boarding,
(d) The affected emergency exit is not used for passenger
boarding, nor for any purpose whilst passengers are on
board,
NOTE: If the affected emergency exit is operative
mechanically, it may still be used for evacuation in
the case of emergency.
(e) Visual indications (illuminated and non-illuminated)
directing passengers to the affected emergency exit are
obscured,
(f) All crew members are briefed on the location and
condition of the affected emergency exit, passenger
distribution and modified cabin safety procedures,
(g) The affected emergency exit and blocked seating layout
are checked before each flight by the relevant cabin
crew member, and
(h) The escape path to the affected emergency exit is
checked by the relevant cabin crew member to be
unobstructed before each takeoff and landing.
NOTE: Reference may be made to UK CAA
FODCOM 8/99 for guidance relating to passenger
number reduction.
-00-30 Passenger and Service
Doors Emergency
Opening Assisting
System
(except ECJ model)
A 4 3 (M) (O) One may be inoperative or missing for a maximum
of 5 flights provided:
(a) Associated door is considered inoperative. Refer to item
52-00-00 Passenger and Service Doors.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 6
DATE: 30 April 2009
PAGE
S52-2
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
(5) Remarks or Exceptions
-21-00 Overwing Escape Hatch
(EMBRAER 190/195
except ECJ model)
A 2 1 (M) (O) One may be inoperative for a maximum of 5 flights
provided:
(a) Remaining main entry doors are fully operational, and,
(b) Associated door is considered inoperative. Refer to
item 52-00-00 Passenger and Service Doors.
-31-20 Fwd (Aft) Cargo Door
Green Indicators - - - All must be operative.
-51-00 Cockpit Security Door
Automatic Locking
System
A 1 0 (M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated,
(b) Mechanical Latch operates normally and is used to lock
the door,
(c) Alternate procedures are established and used for locking
and unlocking the flight deck door using the Mechanical
Latch, and
(d) Repairs are made within four flights.
Note: These dispatch conditions only apply to and from
countries which require secured doors.
B 1 0 (M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated, and no other
locking system is used, and
(b) Alternate procedures are established and used for
access to the flight deck.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S52-3
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
-51-00 Cockpit Security Door
Automatic Locking
System
(Continued)
1) Cockpit Door Control
Panel
a) LOCK Pushbutton
A
B
1
1
0
0
(5) Remarks or Exceptions
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated,
(b) Mechanical Latch operates normally and is used to lock
the door,
(c) Alternate procedures are established and used for
locking and unlocking the flight deck door using the
Mechanical Latch, and
(d) Repairs are made within four flights.
Note: These dispatch conditions only apply to and from
countries which require secured doors.
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated, and no other
locking system is used, and
(b) Alternate procedures are established and used for
access to the flight deck.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S52-4
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
51-00 Cockpit Security Door
Automatic Locking
System
(Continued)
1) Cockpit Door Control
Panel
(Continued)
b) LOCK Pushbutton
Light
c) INHIB Pushbutton
C
A
B
1
1
1
0
0
0
(5) Remarks or Exceptions
May be inoperative provided the LOCK Pushbutton is
verified to operate normally.
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated,
(b) Mechanical Latch operates normally and is used to
lock the door,
(c) Alternate procedures are established and used for
locking and unlocking the flight deck door using
the Mechanical Latch, and
(d) Repairs are made within four flights.
Note: These dispatch conditions only apply to and from
countries which require secured doors.
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated, and no other
locking system is used, and
(b) Alternate procedures are established and used for
access to the flight deck.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 20 February 2004
PAGE
S52-5
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
51-00 Cockpit Security Door
Automatic Locking
System
(Continued)
1) Cockpit Door Control
Panel
(Continued)
d) INHIB Pushbutton
Light
e) UNLOCKED
Annunciator ON
Light
C
C
1
1
0
0
(5) Remarks or Exceptions
May be inoperative provided the INHIBIT Pushbutton is
verified to operate normally.
(O) May be inoperative provided:
(a) Door Chime operates normally, and
(b) The LOCK and INHIBIT Pushbuttons are verified to
operate normally.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S52-6
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
51-00 Cockpit Security Door
Automatic Locking
System (Continued)
2) Flight Attendant
Cockpit Door Control
Panel
a) Emergency Call
Pushbutton
A
B
1
1
0
0
(5) Remarks or Exceptions
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated,
(b) Mechanical Latch operates normally and is used to
lock the door,
(c) Alternate procedures are established and used for
locking and unlocking the flight deck door using the
Mechanical Latch, and
(d) Repairs are made within four flights.
Note: These dispatch conditions only apply to and from
countries which require secured doors.
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated, and no other
locking system is used, and
(b) Alternate procedures are established and used for
access to the flight deck.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 20 February 2004
PAGE
S52-7
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
51-00 Cockpit Security Door
Automatic Locking
System
(Continued)
2) Flight Attendant
Cockpit Door Control
Panel
(Continued)
b) Emergency Call
Pushbutton Light
c) Door Opening
Sequence Inhibited
Red Light
d) Door Unlocked
Green Light
C
C
C
1
1
1
0
0
0
(5) Remarks or Exceptions
(O) May be inoperative provided alternate procedures are
established and used for access to the flight deck.
(O) May be inoperative provided alternate procedures are
established and used for access to the flight deck.
(O) May be inoperative provided alternate procedures are
established and used for access to the flight deck.
(Continued)
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: Revision 5
DATE: 26 November 2007
PAGE
S52-8
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
51-00 Cockpit Security Door
Automatic Locking
System
(Continued)
3) Door Chime
4) Maintenance Lock
5) Mechanical Latch
A
B
D
D
1
1
1
1
0
0
0
0
(5) Remarks or Exceptions
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated,
(b) Mechanical Latch operates normally and is used to
lock the door,
(c) Alternate procedures are established and used for
locking and unlocking the flight deck door using the
Mechanical Latch, and
(d) Repairs are made within four flights.
Note: These dispatch conditions only apply to and from
countries which require secured doors.
(M) (O) May be inoperative provided:
(a) Automatic locking system is deactivated, and no other
locking system is used, and
(b) Alternate procedures are established and used for
access to the flight deck.
AIRCRAFT
EMBRAER 170/175/190/195
REVISION NO: ORIGINAL
DATE: 30 September 2005
PAGE
S52-9
(1) System & Sequence Numbers
Item
(2) Rectification Interval
(3) Number installed
(4) Number required for dispatch
52 Doors
-70-00 Door Position Indication
on MFD and associated
EICAS Message
C
-
-
(5) Remarks or Exceptions
(M) (O) Two may be inoperative provided affected door is
verified closed, latched and locked before each flight.